Title:
Multi-point Optimization of Airfoils

dc.contributor.author Chiguluri, Bhanu S. en_US
dc.contributor.department Aerospace Engineering en_US
dc.date.accessioned 2011-05-11T19:14:23Z
dc.date.available 2011-05-11T19:14:23Z
dc.date.issued 2011-05-09 en_US
dc.description.abstract Many previous studies focused on developing optimum airfoils for steady flight conditions. However, with minimal extensions airfoils could be designed to perform better at the take-off conditions which would result in the efficient take-offs at shorter runways. An inverse design technique called the Modified Garabedian McFadden (MGM) technique was applied to NACA 0012 airfoil which resulted in an airfoil with drag bucket at the normal flight operation conditions. A newly developed optimization technique was applied to the three-element take-off configuration and a configuration that produced higher lift was obtained. Future work could be conducted on extending these design techniques for various airfoil configurations. en_US
dc.description.advisor Ruffin, Stephen - Faculty Mentor ; Sankar, Lakshmi - Faculty Mentor en_US
dc.identifier.uri http://hdl.handle.net/1853/38820
dc.language.iso en_US en_US
dc.publisher Georgia Institute of Technology en_US
dc.subject Take-off optimization en_US
dc.subject Optimization en_US
dc.subject Lift en_US
dc.subject Drag en_US
dc.subject MGM technique en_US
dc.subject Drag bucket en_US
dc.subject Airfoil design en_US
dc.subject Airfoils en_US
dc.subject Aircraft en_US
dc.title Multi-point Optimization of Airfoils en_US
dc.type Text
dc.type.genre Undergraduate Thesis
dspace.entity.type Publication
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.contributor.corporatename College of Engineering
local.contributor.corporatename Undergraduate Research Opportunities Program
local.relation.ispartofseries Undergraduate Research Option Theses
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relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
relation.isOrgUnitOfPublication 0db885f5-939b-4de1-807b-f2ec73714200
relation.isSeriesOfPublication e1a827bd-cf25-4b83-ba24-70848b7036ac
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